Other State of Design

2023-17-09

Joint Aircraft System Conponent (JASC) Code: 2810, Fuel Storage.

(1) This AD applies to hot air balloons, certified in any category, equipped with a Cameron Balloons Ltd. fuel cylinder part number (P/N) CB2990/A (the affected fuel cylinder). (2) The affected fuel cylinder may be installed on hot air balloon medels including, but not limited to, those of the following design approval holders. (i) Aeroster International, Inc..; (ii) Ballonbau Eorner GmbH; (iii) Balony Kubicek spol. s.r.o.; (iv) Cameron Balloons Ltd.; (v) Eagle Balloon Corp.; (vi) JR Aerosports, Ltd. (type certificate previously held by Sundance Balloons (US)); (vii) Lindstrand Balloons Ltd.; and (viii) Michael D. McGrath (type certificate subsequently transferred to Andrew Philip Richardson, Adams Aerostats LLC.

FAA

2023-0165

ATA 72 – Engine – Low Pressure Turbine Stage 1 Blade Assemblies – Inspection / Replacement

Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G and Trent 1000-H engines, all engine serial numbers. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes.

EASA

2021-0009R1

ATA 75 – Air – Modulated Air System Control Valves – Lock-Out / Deactivation

Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3 and Trent 1000-R3 engines, all serial numbers, except those on which Rolls-Royce modification (mod) 75-K778 has been embodied in production, or TRENT 1000 SB 75-K778 has been embodied in service. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes.

EASA

2023-0164

ATA – Pilot’s Operating Handbook – Emergency Procedures – Amendment

TBM 700 aeroplanes, manufacturer serial numbers (MSN) 687 to 1491 inclusive.

EASA

2023-0163

ATA 72 – Engine – Pistons – Oil Analysis / Replacement

Model E4 and E4P engines, all serial numbers (s/n) listed in Table 1, 2, 3 and 4 of the Mandatory Service Bulletin (MSB), as defined in this AD. These engines are known to be installed on, but not limited to, Diamond Aircraft Industries DA 40 NG, DA 42 NG, DA 42 M-NG and DA 62 aeroplanes.

EASA

2020-0005R1

ATA 53 – Fuselage – Windshield Central Lower Node Continuity Fittings – Inspection / Modification

Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, except aeroplanes meeting one of the configuration criteria below: – A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 (i.e. all three) were embodied in production.

EASA

2023-0162

ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 5 – Fuel Airworthiness Limitations – Amendment

Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.

EASA

2019-0069R1

ATA 25 – Equipment / Furnishings – Overhead Stowage Compartments – Modification

Airbus A318-112, A318-121, A318-122, A319-111, A319-112, A319-115, A319-131, A319-132, A319-133, A320-214, A320-216, A320-232, A320-233, A320-251N, A320-271N, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-253N, A321-271N and A321-272N aeroplanes, manufacturer serial numbers as listed in the applicable SB.

EASA

2018-0126R1

ATA 72 – Engine – Low Pressure Turbine Disc Seal Fins and Interstage Seals – Inspection / Replacement / Modification

RB211 Trent 970-84, 970B-84, 972-84, 972B-84, 972E-84, 977-84, 977B-84 and 980-84 engines, all serial numbers, except those that have embodied Rolls-Royce modification (mod) 72-AJ592 in production. These engines are known to be installed on, but not limited to, Airbus A380 aeroplanes.

EASA

2023–14–10

Joint Aircraft System Component (JASC) Code 2510, Flight Compartment Equipment.

(1) This AD applies to: (i) Ipeco Holdings Limited (Ipeco) pilot and co-pilot seats with a part number (P/N) listed in Paragraph 1.A., Planning Information, Tables 1 and 2, of Ipeco Service Bulletin (SB) Number 063–25–14, Revision 00, dated August 14, 2018, and (ii) Ipeco pilot seat P/N 3A063–0099–01–1 and Ipeco co-pilot seat P/N 3A063–0100–01–1. (2) These seats are installed on, but not limited to, ATR–GIE Avions de Transport Régional ATR 42 and ATR 72 airplanes.

FAA

2021-0281R1

ATA – Aircraft Flight Manual / Engine Bleed Air System – Amendment ATA 36 – Pneumatic – Engine Bleed Air System – Maintenance Tasks

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343 and A330-743L aeroplanes, all manufacturer serial numbers.

EASA

2023-0158

ATA 49 – Airborne Auxiliary Power – Auxiliary Power Unit Scroll Housing Assembly – Replacement

Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A330-841, A330-941 and A330-743L aeroplanes, all manufacturer serial numbers (MSN); and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.

EASA